Go-Around; Flying And Landing With One Engine Inoperative For Training Purposes - Kazan Helicopters Mi-17-1V Flight Manual

MI1-17-1B. Flight manual
minimum limit, turn the throttle control twist grip to the leftmost posi-
tion and apply the LG wheel brakes.
Warning: 1. Only the pilots gained necessary
skill
in training flights
are authorized to perform shortened running landing
on fields of limited dimensions.
2. In performing pre-landing deceleration, take special
care to maintain the main rotor speed within the speci-
fied limits.
4.11. Go-around
(1) If it proves impossible to land on a selected field, or the helicopter carry-
ing external load fails to establish hovering out of ground effect, proceed
to go-around, for this purpose smoothly pull up the collective pitch control
lever to advance power up to takeoff and simultaneously push forward
the control stick to accelerate the helicopter.
Upon attainment of a speed of 100 to 120
kmlh
proceed to climb at en-
gine takeoff or maximum continuous power.
4.12. Flying and landing with one engine inoperative for training purposes
One engine runs at idle or is shut down, the operating one comes to
higher power rating ( up to contingency power).
(1) Land the helicopter with one engine inoperative for training purpose on
an even field having safe clearways or on an aerodrome. In so doing, the
helicopter weight should not exceed the normal takeoff weight.
(2) Execute landing approach with one engine inoperative for training pur-
poses with the helicopter headed into the wind or at a crosswind not ex-
ceeding 5
m/s.
(3) At a height of 300 m, before starting the AIt1-9B (APU), switch off the engine
anti-icing system and the dust protection devices if they have been on.
Start the APU.
Observe readings of the APU instruments and illumination of the OIL PRESS
NORMAL (JJ,ABn.MACnA HOPMA), NORMAL SPEED (050POTbl
HOPMA) annunciators to make sure the APU operates normally.
(4) To shut down one engine for training purposes at a high airspeed pro-
ceed as follows below:
(a) At a height of 300 m above the aerodrome the Captain establishes
horizontal flight at an airspeed of 180 to 200 kmlh and calls:
"Be ready to shutdown left (right) engine". Upon this order the Flight
Engineer prepares the respective engine for shutdown. The Pilot-
Navigator increases alertness in monitoring the power plant opera-
tion and maintenance of the main rotor speed.
(b) Move the throttle lever of the engine to be shut down fully down.
This done, the other engine should automatically gain an elevated
power with its throttle lever latched at the midway position.
(c) The Pilot-Navigator notes the time.
(d) Operate the collective pitch control lever to maintain the main rotor
speed within the limits of 95
±
2%.
(e) To set the operating engine to contingency power it is necessary to
set the CONTINGENCY POWER (CP) switch, located on the EEC
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